Piper Lance II - Page 82

MOUNTING
BRACKET
LANCE
11 SERVICE
MANUAL
INSPECT
THIS BOLT
Figure
3-2.
Flap
Control
Cable
Attachment
Bolt
Inspection.
3-10.
INSPECTION
OF
FLAP
CONTROL
CABLE
ATTACHMENT
BOLT.
(Refer
to
Figure
3-2.)
a.
This
inspection
should
be
accomplished
at the
next
100
hours
or
annual
inspection
and
repeated
at
each
500
hours
thereafter.
b.
The
inspection
is required
to
detect
any
possible
wear
and
replacement
of
attachment
bolt,
should
evidence
of
wear
be detected.
c.
Remove
the royalite
flap handle
cover
and
proceed
as follows:
d.
On aircraft
having
the
flap
handle
only,
proceed
as
follows:
1.
Remove
flap
handle
mounting
bracket
attachment
bolts.
2.
Raise
flap
handle
and
bracket
assembly
to
gain
access
to the
control
cable
attachment
bolt.
e.
On
aircraft
having
the
flap handle
and
trim
wheel
mounted
together,
proceed
as
follows:
1.
Loosen
the
trim
wheel
attachment
bolt.
2.
Remove
the trim
wheel
bracket
attachment
bolts
and
remove
bracket
from
top
of tunnel.
3. Remove
flap
handle
mounting
bracket
attachment
bolts
and
raise
handle
and
bracket
assembly
to gain
access
to
control
cable
attachment
bolt.
f.
Remove
and
inspect
cable
attachment
bolt
for possible
wear.
Should
wear
be
detected,
replace
bolt
with
new
AN23-10
clevis
bolt.
g.
Reinstall
all parts
that
were
removed.
Issued:
1/3/78
INSPECTION
1D10